JPH0791297A - Air-fuel ratio controller of internal combustion engine - Google Patents

Air-fuel ratio controller of internal combustion engine

Info

Publication number
JPH0791297A
JPH0791297A JP5234950A JP23495093A JPH0791297A JP H0791297 A JPH0791297 A JP H0791297A JP 5234950 A JP5234950 A JP 5234950A JP 23495093 A JP23495093 A JP 23495093A JP H0791297 A JPH0791297 A JP H0791297A
Authority
JP
Japan
Prior art keywords
fuel ratio
air
sensor
output
downstream
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP5234950A
Other languages
Japanese (ja)
Other versions
JP3134624B2 (en
Inventor
Masahiro Nasu
昌博 那須
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toyota Motor Corp filed Critical Toyota Motor Corp
Priority to JP05234950A priority Critical patent/JP3134624B2/en
Priority to US08/305,641 priority patent/US5475975A/en
Publication of JPH0791297A publication Critical patent/JPH0791297A/en
Application granted granted Critical
Publication of JP3134624B2 publication Critical patent/JP3134624B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/02Circuit arrangements for generating control signals
    • F02D41/14Introducing closed-loop corrections
    • F02D41/1438Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
    • F02D41/1439Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the position of the sensor
    • F02D41/1441Plural sensors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)

Abstract

PURPOSE:To enable a high precision air-fuel ratio control by resolving the problem of response delay of an air-fuel ratio sensor arranged on an exhaust pipe downstream from a catalytic converter. CONSTITUTION:The furture value of a downstream air-fuel ratio sensor after the delay time passes is estimated by the hysteresis of the output of the past fixed period of an upstream air-fuel ratio sensor 13 arranged in an exhaust passage upstream from a catalytic converter 12 and the present output of the downstream air-fuel ratio sensor 15 arranged in the exhaust passage downstream from the catalytic converter, and also the output of the upstream air-fuel ratio sensor 13 is corrected on the basis of this estimated output, so as to perform the air-fuel ratio feedback control. Thereby, the response delay of the downstream air-fuel ratio sensor can be substantially made zero.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、内燃機関の空燃比制御
装置に関し、詳細には排気浄化触媒コンバータの上流側
と下流側とに配置した空燃比センサの出力に基づいて機
関の燃焼空燃比を制御する内燃機関の空燃比制御装置に
関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an air-fuel ratio control system for an internal combustion engine, and more particularly, to a combustion air-fuel ratio of an engine based on the outputs of air-fuel ratio sensors arranged upstream and downstream of an exhaust purification catalytic converter. The present invention relates to an air-fuel ratio control device for an internal combustion engine that controls the engine.

【0002】[0002]

【従来の技術】内燃機関の排気通路に三元触媒コンバー
タを配置し、排気中のNOX 、HC、COの3つの有害
成分を同時に浄化する技術が知られている。また三元触
媒は、流入する排気の空燃比が理論空燃比近傍の極めて
狭い範囲にある場合にのみ上記三成分を同時に浄化可能
であることから、触媒コンバータに流入する排気空燃比
を理論空燃比近傍に維持することが排気性状を良好に保
つ上で重要となる。この目的で、排気通路の触媒コンバ
ータ上流側にO2 センサ等の空燃比センサを設けて実際
に触媒コンバータに流入する排気空燃比を検出するとと
もに、検出した排気空燃比に基づいて排気空燃比を理論
空燃比に維持するように機関への燃料供給量をフィード
バック制御することが一般に行われている。(なお、本
明細書中では、触媒コンバータ上流側の排気通路、及び
機関燃焼室、吸気通路等に供給された空気の量と燃料の
量との比を排気空燃比と呼び、機関燃焼室内における燃
焼の空燃比を燃焼空燃比と呼ぶこととする。従って触媒
コンバータ上流側の排気通路に燃料または二次空気が供
給されない場合には、排気空燃比と燃焼空燃比とは一致
することになる。)ところが、上述のように、触媒コン
バータ上流側に設けた空燃比センサの出力信号に応じて
機関燃焼空燃比を制御すると、実際には問題を生じる場
合がある。
2. Description of the Related Art There is known a technique in which a three-way catalytic converter is arranged in an exhaust passage of an internal combustion engine to purify three harmful components of NO x , HC and CO in the exhaust gas at the same time. Further, the three-way catalyst can purify the above three components simultaneously only when the air-fuel ratio of the inflowing exhaust gas is in an extremely narrow range near the stoichiometric air-fuel ratio. Maintaining the vicinity is important for maintaining good exhaust properties. For this purpose, an air-fuel ratio sensor such as an O 2 sensor is provided on the upstream side of the catalytic converter in the exhaust passage to detect the exhaust air-fuel ratio actually flowing into the catalytic converter, and the exhaust air-fuel ratio is adjusted based on the detected exhaust air-fuel ratio. Feedback control of the fuel supply amount to the engine is generally performed so as to maintain the stoichiometric air-fuel ratio. (In this specification, the ratio of the amount of air and the amount of fuel supplied to the exhaust passage on the upstream side of the catalytic converter, the engine combustion chamber, the intake passage, etc. is called the exhaust air-fuel ratio, and The air-fuel ratio of combustion is referred to as the combustion air-fuel ratio, and therefore, when fuel or secondary air is not supplied to the exhaust passage upstream of the catalytic converter, the exhaust air-fuel ratio and the combustion air-fuel ratio match. However, when the engine combustion air-fuel ratio is controlled according to the output signal of the air-fuel ratio sensor provided on the upstream side of the catalytic converter as described above, a problem may actually occur.

【0003】すなわち、上述のような制御を行うと個々
の空燃比センサの出力特性のばらつきが直接制御に反映
されてしまうため、空燃比制御の精度が悪化する場合が
生じる。また、触媒コンバータ上流側では各気筒から排
出された排気ガスが均一に混合しておらず、上流側空燃
比センサの配置によってはセンサが特定の気筒の排気空
燃比変動を検出してしまうため、全体として触媒コンバ
ータに流入する排気空燃比を正確に理論空燃比近傍に制
御することが困難な場合がある。更に、触媒コンバータ
上流側では排気温度が高く空燃比センサが劣化し易いた
め、劣化によりセンサ出力特性が経年変化した場合にも
同様な問題が生じる。
That is, when the above-mentioned control is performed, variations in the output characteristics of the individual air-fuel ratio sensors are directly reflected in the control, so that the accuracy of the air-fuel ratio control may deteriorate. Further, the exhaust gas discharged from each cylinder is not uniformly mixed on the upstream side of the catalytic converter, and depending on the arrangement of the upstream side air-fuel ratio sensor, the sensor detects the exhaust air-fuel ratio fluctuation of a specific cylinder. As a whole, it may be difficult to accurately control the exhaust air-fuel ratio flowing into the catalytic converter to be close to the stoichiometric air-fuel ratio. Further, since the exhaust gas temperature is high on the upstream side of the catalytic converter and the air-fuel ratio sensor is easily deteriorated, the same problem occurs even when the sensor output characteristics change over time due to the deterioration.

【0004】この問題を解決するために、上流側空燃比
センサの他に触媒コンバータの下流側の排気通路にも空
燃比センサ(下流側空燃比センサ)を配置し、上流側空
燃比センサの出力信号に基づく空燃比制御に加えて、下
流側空燃比センサの出力に基づいて空燃比制御を行うよ
うにした、いわゆるダブルセンサシステムが提案されて
いる(特開昭63−195351号公報参照)。
To solve this problem, in addition to the upstream air-fuel ratio sensor, an air-fuel ratio sensor (downstream air-fuel ratio sensor) is also arranged in the exhaust passage on the downstream side of the catalytic converter, and the output of the upstream air-fuel ratio sensor is set. A so-called double sensor system has been proposed in which, in addition to signal-based air-fuel ratio control, air-fuel ratio control is performed based on the output of a downstream side air-fuel ratio sensor (see Japanese Patent Laid-Open No. 63-195351).

【0005】触媒コンバータ下流側では、各気筒からの
排気は均一に混合されているため、下流側空燃比センサ
が特定気筒の影響を受けることが少なく、また排気ガス
温度も上流側に較べて低くなっているためセンサの劣化
による出力特性の変化も少ない。このため、ダブルセン
サシステムにおいては、下流側空燃比センサ出力に基づ
いて上流側空燃比センサによる空燃比フィードバック制
御を補正することにより、上流側空燃比センサの出力特
性の経年変化やばらつきによる空燃比制御のずれは下流
側空燃比センサにより補正され、より正確な空燃比制御
が行われる。
On the downstream side of the catalytic converter, since the exhaust gas from each cylinder is uniformly mixed, the downstream side air-fuel ratio sensor is less affected by the specific cylinder, and the exhaust gas temperature is lower than that on the upstream side. As a result, there is little change in output characteristics due to sensor deterioration. Therefore, in the double sensor system, by correcting the air-fuel ratio feedback control by the upstream air-fuel ratio sensor based on the output of the downstream air-fuel ratio sensor, the air-fuel ratio due to the secular change or variation in the output characteristics of the upstream air-fuel ratio sensor The control deviation is corrected by the downstream air-fuel ratio sensor, and more accurate air-fuel ratio control is performed.

【0006】[0006]

【発明が解決しようとする課題】ところが、ダブルセン
サシステムでは、三元触媒のO2 ストレージ作用のた
め、下流側空燃比センサでは上流側空燃比センサに較べ
て空燃比変化の検出が遅れる問題がある。一般に三元触
媒は、排気空燃比が理論空燃比より大きい時に(リーン
空燃比の時に)排気中の酸素を吸着し、排気空燃比が理
論空燃比より小さい時に(リッチ空燃比の時に)吸着し
た酸素を放出する、いわゆるO2 ストレージ作用を有し
ている。このO2 ストレージ作用により、三元触媒コン
バータに流入する排気空燃比が短時間理論空燃比から外
れた場合でも三元触媒の雰囲気の空燃比を理論空燃比近
傍に保持することができ、三元触媒の排気浄化性能を良
好に維持することが可能となるが、その反面、三元触媒
の酸素の吸着、放出作用のため触媒コンバータ下流側で
の排気空燃比の変化は上流側の排気空燃比変化より遅れ
て生じる。
However, in the double sensor system, the downstream side air-fuel ratio sensor has a problem that the detection of the air-fuel ratio change is delayed as compared with the upstream side air-fuel ratio sensor due to the O 2 storage action of the three-way catalyst. is there. Generally, a three-way catalyst adsorbs oxygen in the exhaust when the exhaust air-fuel ratio is larger than the theoretical air-fuel ratio (when the air-fuel ratio is lean), and when the exhaust air-fuel ratio is smaller than the theoretical air-fuel ratio (when the air-fuel ratio is rich). It has a so-called O 2 storage function of releasing oxygen. Due to this O 2 storage action, even if the exhaust air-fuel ratio flowing into the three-way catalytic converter deviates from the stoichiometric air-fuel ratio for a short time, the air-fuel ratio of the atmosphere of the three-way catalyst can be maintained near the stoichiometric air-fuel ratio. It is possible to maintain good exhaust purification performance of the catalyst, but on the other hand, changes in the exhaust air-fuel ratio on the downstream side of the catalytic converter due to the adsorption and release of oxygen by the three-way catalyst cause changes in the exhaust air-fuel ratio on the upstream side. It occurs later than the change.

【0007】例えば、触媒コンバータ入口側の排気空燃
比が理論空燃比近傍でリーンからリッチに変化したよう
な場合でも、触媒コンバータ出口側の排気空燃比は三元
触媒に貯蔵された酸素が放出されている間は直ちには変
化せず、三元触媒に貯蔵された酸素が放出され尽くした
後に、すなわちある程度の時間遅れの後にリッチ側に変
化することになる。従って、理論空燃比近傍で空燃比を
制御中に何らかの原因で、例えば排気空燃比がリッチ空
燃比側に移行し始めたような場合、下流側空燃比センサ
が空燃比のリッチ側への移行を検出した時点では、上流
側の排気空燃比は既に大きくリッチ側にずれてしまって
いることになり、排気空燃比を精度よく理論空燃比近傍
に制御することが困難になる。また、リッチ空燃比から
リーン空燃比への変化の際にも同様な時間遅れが生じ
る。
For example, even when the exhaust air-fuel ratio on the inlet side of the catalytic converter changes from lean to rich near the stoichiometric air-fuel ratio, the exhaust air-fuel ratio on the outlet side of the catalytic converter releases oxygen stored in the three-way catalyst. It does not change immediately during the operation, but changes to the rich side after the oxygen stored in the three-way catalyst is exhausted, that is, after a certain time delay. Therefore, for some reason while controlling the air-fuel ratio near the stoichiometric air-fuel ratio, for example, when the exhaust air-fuel ratio starts to shift to the rich air-fuel ratio side, the downstream side air-fuel ratio sensor shifts to the rich side of the air-fuel ratio. At the time of detection, the exhaust air-fuel ratio on the upstream side has already largely shifted to the rich side, and it becomes difficult to control the exhaust air-fuel ratio accurately near the stoichiometric air-fuel ratio. Also, a similar time delay occurs when changing from the rich air-fuel ratio to the lean air-fuel ratio.

【0008】上述の特開昭63−195351号公報の
ダブルセンサシステムでは、この下流側空燃比センサの
空燃比変化検出の時間遅れの問題を解決するために、下
流側空燃比センサの検出した空燃比と理論空燃比との偏
差が大きいほど上流側空燃比センサによるフィードバッ
ク制御の制御定数の単位時間当たりの更新量を大きくす
ることにより空燃比が理論空燃比に収束する時間の短縮
を図っている。しかし、同公報のダブルセンサシステム
では、依然としてある程度の時間遅れを伴って検出され
た現在の下流側空燃比センサの出力を用いて制御定数の
更新量を決定することになるため、例えば下流側空燃比
センサの出力が同一であれば、上流側の空燃比がリッチ
側に移行中かリーン側に移行中かとは無関係に更新量が
決定されてしまうことになる。このため、上記公報のダ
ブルセンサシステムでは必ずしも空燃比変化傾向を反映
した応答性の良い空燃比制御が行われない問題がある。
In the double sensor system of Japanese Patent Laid-Open No. 63-195351 mentioned above, in order to solve the problem of time delay in detecting the air-fuel ratio change of the downstream side air-fuel ratio sensor, the air detected by the downstream side air-fuel ratio sensor is solved. The larger the deviation between the fuel ratio and the stoichiometric air-fuel ratio, the larger the update amount of the control constant of the feedback control by the upstream air-fuel ratio sensor per unit time is to shorten the time for the air-fuel ratio to converge to the stoichiometric air-fuel ratio. . However, in the double sensor system of the publication, since the update amount of the control constant is determined using the output of the current downstream side air-fuel ratio sensor which is still detected with a certain time delay, for example, the downstream side air If the outputs of the fuel ratio sensors are the same, the update amount will be determined regardless of whether the upstream air-fuel ratio is shifting to the rich side or the lean side. Therefore, in the double sensor system of the above publication, there is a problem that the responsive air-fuel ratio control reflecting the air-fuel ratio change tendency is not always performed.

【0009】本発明は、上記問題に鑑み、下流側空燃比
センサ出力の上記時間遅れにより生じる問題を解決し、
制御の応答性を向上させ、高精度の空燃比制御を可能と
する空燃比制御装置を提供することを目的としている。
In view of the above problems, the present invention solves the problems caused by the time delay of the output of the downstream side air-fuel ratio sensor,
An object of the present invention is to provide an air-fuel ratio control device that improves control response and enables highly accurate air-fuel ratio control.

【0010】[0010]

【課題を解決するための手段】本発明によれば図1の本
発明の構成図に示すように、内燃機関の排気通路に配置
された三元触媒Aと、該三元触媒の上流側排気通路に配
置され排気空燃比に応じた出力信号を発生する上流側空
燃比センサBと、前記三元触媒Aの下流側排気通路に配
置され排気空燃比に応じた出力信号を発生する下流側空
燃比センサCと、前記上流側空燃比センサBの出力信号
の過去所定期間の変化履歴と、前記下流側空燃比センサ
Cの現在の出力信号とに基づいて、現在から所定時間経
過後の前記下流側空燃比センサCの出力信号の将来値を
推定する推定手段Dと、前記推定された下流側空燃比セ
ンサCの出力信号に基づいて前記上流側空燃比センサB
の現在の出力を補正する補正手段Eと、前記補正された
上流側空燃比センサBの出力に基づいて前記内燃機関の
燃焼空燃比を制御する制御手段Fとを備えた内燃機関の
空燃比制御装置が提供される。
According to the present invention, as shown in the block diagram of the present invention in FIG. 1, a three-way catalyst A disposed in an exhaust passage of an internal combustion engine and an exhaust gas on the upstream side of the three-way catalyst. An upstream air-fuel ratio sensor B which is disposed in the passage and generates an output signal according to the exhaust air-fuel ratio, and a downstream air which is disposed in the downstream exhaust passage of the three-way catalyst A and generates an output signal according to the exhaust air-fuel ratio. Based on the history of changes in the output signals of the fuel ratio sensor C, the upstream air-fuel ratio sensor B in the past predetermined period, and the current output signal of the downstream air-fuel ratio sensor C, the downstream after a predetermined time has elapsed from the present time. Estimating means D for estimating a future value of the output signal of the side air-fuel ratio sensor C, and the upstream side air-fuel ratio sensor B based on the estimated output signal of the downstream side air-fuel ratio sensor C.
Of the internal combustion engine, and a control means F for controlling the combustion air-fuel ratio of the internal combustion engine based on the corrected output of the upstream side air-fuel ratio sensor B. A device is provided.

【0011】[0011]

【作用】三元触媒A下流側の排気空燃比は、三元触媒の
2 ストレージ作用のために、三元触媒A上流側の排気
空燃比に変化が生じてから或る遅れ時間が経過した後に
同様な変化を開始する。従って、現時点での三元触媒A
上流側の排気空燃比の変化状況を知れば、上記遅れ時間
経過後の三元触媒A下流側の排気空燃比変化を予測する
ことが可能である。
The exhaust air-fuel ratio on the downstream side of the three-way catalyst A has a certain delay time since the exhaust air-fuel ratio on the upstream side of the three-way catalyst A changes due to the O 2 storage function of the three-way catalyst. Later a similar change begins. Therefore, the current three-way catalyst A
By knowing the change state of the exhaust air-fuel ratio on the upstream side, it is possible to predict the change of the exhaust air-fuel ratio on the downstream side of the three-way catalyst A after the delay time has elapsed.

【0012】本発明の推定手段Dは、上流側空燃比セン
サBの出力信号の過去所定期間の変化履歴から三元触媒
A上流側での排気空燃比変化状況を検出して、この変化
状況と現在の下流側空燃比センサCの出力信号(すなわ
ち現在の三元触媒下流側排気空燃比)とに基づいて、現
在から、上記遅れ時間に相当する時間が経過した時点で
の下流側空燃比センサCの出力信号(排気空燃比)を推
定する。
The estimating means D of the present invention detects the change state of the exhaust air-fuel ratio on the upstream side of the three-way catalyst A from the change history of the output signal of the upstream side air-fuel ratio sensor B in the past predetermined period, and detects the change state. Based on the current output signal of the downstream side air-fuel ratio sensor C (that is, the current three-way catalyst downstream side exhaust air-fuel ratio), the downstream side air-fuel ratio sensor at the time when the time corresponding to the delay time has elapsed from the present time The output signal of C (exhaust air-fuel ratio) is estimated.

【0013】補正手段Eは、下流側空燃比センサCの現
在の出力信号ではなく、上記により推定された将来の下
流側空燃比センサCの出力信号に基づいて上流側空燃比
センサBの出力を補正する。制御手段Fは、この補正さ
れた上流側空燃比センサBの出力信号に基づいて機関燃
焼空燃比を制御するため、下流側空燃比センサCの出力
信号による空燃比の補正の際に時間遅れが生じない。
The correcting means E determines the output of the upstream side air-fuel ratio sensor B based on not the present output signal of the downstream side air-fuel ratio sensor C but the future output signal of the downstream side air-fuel ratio sensor C estimated as described above. to correct. Since the control means F controls the engine combustion air-fuel ratio based on the corrected output signal of the upstream side air-fuel ratio sensor B, there is a time delay when the air-fuel ratio is corrected by the output signal of the downstream side air-fuel ratio sensor C. Does not happen.

【0014】[0014]

【実施例】図2は本発明に係る空燃比制御装置を適用し
た内燃機関の一実施例を示す全体概略図である。図2に
おいて、機関本体1の吸気通路2にはエアフローメータ
3が設けられている。エアフローメータ3は吸入空気量
を直接計測するものであって、たとえばポテンショメー
タを内蔵した可動ベーン式エアフローメータ等が使用さ
れ、吸入空気量に比例したアナログ電圧の出力信号を発
生する。この出力信号は制御回路10のマルチプレクサ
内蔵A/D変換器101に入力されている。ディストリ
ビュータ4には、その軸がたとえばクランク角に換算し
て720°毎に基準位置検出用パルス信号を発生するク
ランク角センサ5、およびクランク角に換算して30°
毎にクランク各検出用パルス信号を発生するクランク角
センサ6がそれぞれ設けられている。これらクランク角
センサ5、6のパルス信号は制御回路10の入出力イン
ターフェイス102に供給され、このうちクランク角セ
ンサ6の出力はCPU103の割込み端子に供給され
る。
FIG. 2 is an overall schematic view showing an embodiment of an internal combustion engine to which the air-fuel ratio control device according to the present invention is applied. In FIG. 2, an air flow meter 3 is provided in the intake passage 2 of the engine body 1. The air flow meter 3 is a device for directly measuring the intake air amount. For example, a movable vane type air flow meter having a built-in potentiometer is used, and an output signal of an analog voltage proportional to the intake air amount is generated. This output signal is input to the A / D converter 101 with a built-in multiplexer of the control circuit 10. The distributor 4 has its axis converted into, for example, a crank angle, a crank angle sensor 5 that generates a reference position detecting pulse signal every 720 °, and a crank angle of 30 °.
A crank angle sensor 6 that generates a pulse signal for detecting each crank is provided for each. The pulse signals of the crank angle sensors 5 and 6 are supplied to the input / output interface 102 of the control circuit 10, and the output of the crank angle sensor 6 is supplied to the interrupt terminal of the CPU 103.

【0015】さらに、吸気通路2には各気筒毎に燃料供
給系から加圧燃料を吸気ポートへ供給するための燃料噴
射弁7が設けられている。また、機関本体1のシリンダ
ブロックのウォータジャケット8には、冷却水の温度を
検出するための水温センサ9が設けられている。水温セ
ンサ9は冷却水の温度に応じたアナログ電圧の電気信号
を発生する。この出力もA/D変換器101に供給され
ている。
Further, the intake passage 2 is provided with a fuel injection valve 7 for supplying pressurized fuel from the fuel supply system to the intake port for each cylinder. The water jacket 8 of the cylinder block of the engine body 1 is provided with a water temperature sensor 9 for detecting the temperature of the cooling water. The water temperature sensor 9 generates an electric signal of analog voltage according to the temperature of the cooling water. This output is also supplied to the A / D converter 101.

【0016】排気マニホールド11より下流の排気系に
は、排気ガス中の3つの有害成分HC、CO、NOxを
同時に浄化する三元触媒を収容する触媒コンバータ12
が設けられている。排気マニホールド11には、すなわ
ち触媒コンバータ12の上流側には第1の空燃比センサ
(上流側空燃比センサ)13が設けられ、触媒コンバー
タ12の下流側の排気管14には第2の空燃比センサ
(下流側空燃比センサ)15が設けられている。
In the exhaust system downstream of the exhaust manifold 11, a catalytic converter 12 containing a three-way catalyst for simultaneously purifying three harmful components HC, CO and NOx in the exhaust gas.
Is provided. A first air-fuel ratio sensor (upstream air-fuel ratio sensor) 13 is provided in the exhaust manifold 11, that is, upstream of the catalytic converter 12, and a second air-fuel ratio is provided in the exhaust pipe 14 downstream of the catalytic converter 12. A sensor (downstream air-fuel ratio sensor) 15 is provided.

【0017】本実施例では、上流側空燃比センサ13と
しては、排気中の酸素成分濃度と広い空燃比範囲で一対
一に対応する、つまり排気空燃比と一対一に対応する出
力信号を発生する全域空燃比センサ(A/Fセンサ)が
使用されている。A/Fセンサとしては、いくつかのタ
イプがある。図6は一般的なA/Fセンサの構造を模式
的に示している。A/Fセンサ210は、白金電極21
1、212の間にジルコニア等の固体電解質213を配
置し、陰極(排気側電極)212面上に排気ガス中の酸
素分子の陰極への到達を制限するセラミックコーティン
グ層よりなる拡散律速層214を設けた構造となってい
る。図6のA/Fセンサにおいて、陰極212を排気ガ
スに接するように配置し、陽極211を大気に接するよ
うに配置するとともに或る一定温度以上で両電極21
1、212間に電圧を印加すると、陰極212側では排
気中の酸素分子がイオン化され、イオン化した酸素分子
が固体電解質213内を陽極211に向かって移動して
陽極211で再び酸素分子になる酸素ポンプ作用を生じ
る。この酸素ポンプ作用により、電極211、212間
には単位時間に移動した酸素分子の量に比例する電流が
流れる。しかし、拡散律速層214により陰極への酸素
分子の到達が制限されるため、この出力電流は或る一定
値で飽和し、電圧を上げても電流は増加しなくなる。ま
た、この飽和電流の値は排気中の酸素濃度に略比例す
る。従って、印加電圧を適当に設定することにより、酸
素濃度と略比例する出力電流を得ることができる。本実
施例では、この出力電流は電圧信号に変換され、制御回
路10のA/D変換器101に供給される。排気中の酸
素濃度と空燃比とは一対一の相関があるので、上記出力
電圧は排気空燃比と一対一の相関を持ち、上記出力電流
により排気空燃比を知ることができる。図7は本実施例
で使用するA/Fセンサ13の出力特性を示している。
In the present embodiment, the upstream side air-fuel ratio sensor 13 generates an output signal which corresponds to the oxygen component concentration in the exhaust gas in a wide air-fuel ratio range, that is, in one-to-one correspondence with the exhaust air-fuel ratio. A full range air-fuel ratio sensor (A / F sensor) is used. There are several types of A / F sensors. FIG. 6 schematically shows the structure of a general A / F sensor. The A / F sensor 210 has a platinum electrode 21.
A solid electrolyte 213 such as zirconia is arranged between the first and the second 212, and a diffusion-controlling layer 214 made of a ceramic coating layer that restricts oxygen molecules in the exhaust gas from reaching the cathode is disposed on the surface of the cathode (exhaust-side electrode) 212. It has a structure provided. In the A / F sensor of FIG. 6, the cathode 212 is placed in contact with the exhaust gas, the anode 211 is placed in contact with the atmosphere, and both electrodes 21 are placed at a certain temperature or higher.
When a voltage is applied between Nos. 1 and 212, oxygen molecules in the exhaust gas are ionized on the cathode 212 side, and the ionized oxygen molecules move in the solid electrolyte 213 toward the anode 211 and become oxygen molecules again at the anode 211. It produces a pumping action. Due to this oxygen pumping action, a current flows between the electrodes 211 and 212 in proportion to the amount of oxygen molecules moved per unit time. However, since the diffusion rate controlling layer 214 restricts the oxygen molecules from reaching the cathode, the output current is saturated at a certain constant value, and the current does not increase even if the voltage is increased. The value of this saturation current is approximately proportional to the oxygen concentration in the exhaust gas. Therefore, by appropriately setting the applied voltage, it is possible to obtain an output current approximately proportional to the oxygen concentration. In this embodiment, this output current is converted into a voltage signal and supplied to the A / D converter 101 of the control circuit 10. Since the oxygen concentration in the exhaust and the air-fuel ratio have a one-to-one correlation, the output voltage has a one-to-one correlation with the exhaust air-fuel ratio, and the exhaust air-fuel ratio can be known from the output current. FIG. 7 shows the output characteristics of the A / F sensor 13 used in this embodiment.

【0018】一方、本実施例では下流側空燃比センサ1
5としては、A/Fセンサと同様に排気中の酸素濃度に
応じた電圧信号を出力するが、理論空燃比を中心として
出力電圧が比較的急激に変化する、いわゆるO2 センサ
が使用される。O2 センサは図6に示したA/Fセンサ
と略同一の構造であるが、図6の拡散律速層214が設
けられておらず、電極211、212間を開放した状態
で使用される。この状態で固体電解質213が排気ガス
にさらされて温度が上昇すると、A/Fセンサの場合と
は逆に大気側(高酸素濃度側)電極211から排気側
(低酸素濃度側)電極212に向けて酸素イオンの移動
が生じるため、電極211、212間には大気側と排気
側の酸素濃度の相違に対応した電圧が発生する。また、
排気中の酸素濃度は理論空燃比を境にリッチ側とリーン
側とで急激に変化するため、O2 センサの出力は図8に
示すように理論空燃比近傍で比較的急激に変化する、い
わゆるZ特性を示している。
On the other hand, in this embodiment, the downstream air-fuel ratio sensor 1
As 5, a so-called O 2 sensor is used, which outputs a voltage signal according to the oxygen concentration in the exhaust gas as with the A / F sensor, but the output voltage changes relatively rapidly around the theoretical air-fuel ratio. . The O 2 sensor has substantially the same structure as the A / F sensor shown in FIG. 6, but the diffusion rate controlling layer 214 of FIG. 6 is not provided, and the O 2 sensor is used with the electrodes 211 and 212 opened. When the solid electrolyte 213 is exposed to the exhaust gas and the temperature rises in this state, the atmosphere side (high oxygen concentration side) electrode 211 moves to the exhaust side (low oxygen concentration side) electrode 212, contrary to the case of the A / F sensor. Since oxygen ions are moved toward the electrodes, a voltage corresponding to the difference in oxygen concentration between the atmosphere side and the exhaust side is generated between the electrodes 211 and 212. Also,
Since the oxygen concentration in the exhaust gas abruptly changes between the rich side and the lean side with the stoichiometric air-fuel ratio as a boundary, the output of the O 2 sensor changes relatively abruptly near the stoichiometric air-fuel ratio as shown in FIG. The Z characteristic is shown.

【0019】本実施例では、上流側空燃比センサの出力
を下流側空燃比センサの出力を用いて補正する制御を行
っていること、及び前記時間遅れの問題に関連して下流
側空燃比センサの応答速度ができるだけ速いことが望ま
しいことなどから、A/Fセンサに較べて基準出力電圧
(理論空燃比相当出力電圧)の経年変化が少なく応答性
の良いO2 センサを下流側空燃比センサ15として使用
している。なお、以下の説明では上流側空燃比センサを
A/Fセンサ13、下流側空燃比センサをO2センサ1
5と呼び、これらを区別することとする。
In this embodiment, the control of correcting the output of the upstream side air-fuel ratio sensor using the output of the downstream side air-fuel ratio sensor is performed, and the downstream side air-fuel ratio sensor is related to the problem of the time delay. Since it is desirable that the response speed of the A / F sensor be as fast as possible, the downstream side air-fuel ratio sensor 15 should be an O 2 sensor that has less aging change of the reference output voltage (theoretical air-fuel ratio equivalent output voltage) than the A / F sensor and has good response. Is used as. In the following description, the upstream air-fuel ratio sensor is the A / F sensor 13, and the downstream air-fuel ratio sensor is the O 2 sensor 1.
We will call them 5 and distinguish them.

【0020】本実施例では、制御回路10は、たとえば
マイクロコンピュータとして構成され、A/D変換器1
01、入出力インターフェイス102、CPU103の
外に、RAM104、ROM105、クロック発生回路
107等が設けられている。本実施例では、制御回路1
0は、機関1の燃料噴射制御、点火時期制御等の基本制
御を行う他、後述のように請求項1に記載した推定手
段、補正手段、制御手段として機能し、機関1の空燃比
制御を行う。
In this embodiment, the control circuit 10 is configured as, for example, a microcomputer, and the A / D converter 1 is used.
A RAM 104, a ROM 105, a clock generation circuit 107, and the like are provided outside the 01, the input / output interface 102, and the CPU 103. In this embodiment, the control circuit 1
0 performs basic control such as fuel injection control and ignition timing control of the engine 1, and also functions as an estimation unit, a correction unit, and a control unit described in claim 1 as described later, and controls the air-fuel ratio of the engine 1. To do.

【0021】また、吸気通路2のスロットル弁16に
は、スロットル弁16が全閉状態か否かを示す信号、す
なわちLL信号を発生するアイドルスイッチ17が設け
られている。このアイドル状態出力信号LLは制御回路
10の入出力インターフェイス102に供給される。1
8は2次空気導入吸気弁であって、減速時あるいはアイ
ドル時に図示しないエアポンプ等の空気源から2次空気
を排気管11に供給して、HC、COエミッションを低
減するためのものである。
Further, the throttle valve 16 of the intake passage 2 is provided with an idle switch 17 for generating a signal indicating whether or not the throttle valve 16 is fully closed, that is, an LL signal. The idle state output signal LL is supplied to the input / output interface 102 of the control circuit 10. 1
Reference numeral 8 denotes a secondary air introduction intake valve, which supplies secondary air from an air source such as an air pump (not shown) to the exhaust pipe 11 during deceleration or idling to reduce HC and CO emissions.

【0022】さらに、制御回路10において、ダウンカ
ウンタ108、フリップフロップ109、および駆動回
路110は燃料噴射弁7を制御するためのものである。
すなわち、後述のルーチンにおいて、燃料噴射量(噴射
時間)fiが演算されると、噴射時間fiがダウンカウ
ンタ108にプリセットされると共にフリップフロップ
109もセットされる。この結果、駆動回路110が燃
料噴射弁7の付勢を開始する。他方、ダウンカウンタ1
08がクロック信号(図示せず)を計数して最後にその
出力端子が“1”レベルとなったときに、フリップフロ
ップ109がセットされて駆動回路110は燃料噴射弁
7の付勢を停止する。つまり、上述の燃料噴射時間fi
だけ燃料噴射弁7は付勢され、時間fiに応じた量の燃
料が機関本体1の燃焼室に送り込まれることになる。
Furthermore, in the control circuit 10, the down counter 108, the flip-flop 109, and the drive circuit 110 are for controlling the fuel injection valve 7.
That is, in the routine described later, when the fuel injection amount (injection time) fi is calculated, the injection time fi is preset in the down counter 108 and the flip-flop 109 is also set. As a result, the drive circuit 110 starts energizing the fuel injection valve 7. On the other hand, down counter 1
08 counts a clock signal (not shown), and when the output terminal finally becomes "1" level, the flip-flop 109 is set and the drive circuit 110 stops the energization of the fuel injection valve 7. . That is, the above fuel injection time fi
Only then, the fuel injection valve 7 is energized, and an amount of fuel corresponding to the time fi is sent to the combustion chamber of the engine body 1.

【0023】なお、CPU103の割込み発生は、A/
D変換器101のA/D変換終了後、入出力インターフ
ェイス102がクランク角センサ6のパルス信号を受信
した時、等である。エアフローメータ3の吸入空気量デ
ータおよび冷却水温データは所定時間もしくは所定クラ
ンク角毎に実行されるA/D変換ルーチンによって取込
まれてRAM105の所定領域に格納される。つまり、
RAM105における吸入空気量データおよび冷却水温
データは所定時間毎に更新されている。また、回転速度
データはクランク角センサ6の30°CA(クランク
角)毎の割込みによって演算されてRAM105の所定
領域に格納される。
Incidentally, the interrupt generation of the CPU 103 is A /
For example, when the input / output interface 102 receives the pulse signal of the crank angle sensor 6 after the A / D conversion of the D converter 101 is completed. The intake air amount data and the cooling water temperature data of the air flow meter 3 are fetched by an A / D conversion routine executed at a predetermined time or at a predetermined crank angle and stored in a predetermined area of the RAM 105. That is,
The intake air amount data and the cooling water temperature data in the RAM 105 are updated every predetermined time. Further, the rotation speed data is calculated by interruption of the crank angle sensor 6 for each 30 ° CA (crank angle) and stored in a predetermined area of the RAM 105.

【0024】前述のように、本発明による実施例では制
御回路10は請求項1の推定手段として、下流側O2
ンサ15の出力の将来値の予測を行う。以下、図3を用
いて制御回路10による下流側O2 センサ15の出力信
号の予測方法について説明する。図3は、触媒コンバー
タ上流側の排気空燃比A/Fが理論空燃比近傍でリーン
空燃比からリッチ空燃比にステップ状に変化した場合の
下流側O2 センサ15出力電圧VO2の時間的変化を示す
図である。図3では、A/Fは図にで示す時刻までは
リッチ空燃比に維持されており、時刻でリッチ空燃比
からリーン空燃比に急変している。この場合、下流側O
2 センサ15の出力電圧VO2は、三元触媒のO2 ストレ
ージ作用のため、上記時刻から遅れ時間dだけ経過し
た時刻′に達するまではリッチ側出力(約0.9 ボル
ト)に保たれ、時刻′以後は三元触媒に貯蔵された酸
素が放出され尽くされるにつれてリーン出力(約0.1 ボ
ルト)に変化する。
As described above, in the embodiment according to the present invention, the control circuit 10 as the estimating means of claim 1 predicts the future value of the output of the downstream O 2 sensor 15. Hereinafter, a method of predicting the output signal of the downstream O 2 sensor 15 by the control circuit 10 will be described with reference to FIG. FIG. 3 shows the temporal change of the output voltage V O2 of the downstream O 2 sensor 15 when the exhaust air-fuel ratio A / F on the upstream side of the catalytic converter changes stepwise from the lean air-fuel ratio to the rich air-fuel ratio near the stoichiometric air-fuel ratio. FIG. In FIG. 3, the A / F is maintained at the rich air-fuel ratio until the time indicated by, and at the time, the rich air-fuel ratio suddenly changes to the lean air-fuel ratio. In this case, the downstream side O
The output voltage V O2 of the 2 sensor 15 is kept at the rich side output (about 0.9 volt) until the time ′, which is a delay time d from the above time, is reached due to the O 2 storage action of the three-way catalyst. After that, as the oxygen stored in the three-way catalyst is exhausted, it changes to a lean output (about 0.1 volt).

【0025】変化直後の時刻における下流側O2 セン
サ15の出力VO2は上流側排気空燃比A/Fがリーン側
に変化しているにもかかわらずリッチ出力のままになっ
ており、時刻の上流側排気空燃比A/Fに相当する出
力が得られるのは、時刻から時間dだけ経過した時刻
′になった時である。従って、時刻における上流側
空燃比A/Fを下流側O2 センサ15で検出するために
は、時刻の下流側O2 センサ15出力ではなく、時間
dだけ将来の時刻′の下流側O2 センサ15の出力を
用いなければならないことになり、時刻における下流
側O2 センサ15の出力からは時刻における上流側空
燃比A/Fを知ることはできない。
The output V O2 of the downstream O 2 sensor 15 at the time immediately after the change remains a rich output even though the upstream side exhaust air-fuel ratio A / F changes to the lean side. The output corresponding to the upstream side exhaust air-fuel ratio A / F is obtained at time ', which is the time d elapsed from the time. Thus, the downstream O 2 sensor for detecting the upstream-side air-fuel ratio A / F at time downstream O 2 sensor 15 is not the downstream O 2 sensor 15 outputs a time, a future time by the time d ' Since the output of 15 must be used, the upstream air-fuel ratio A / F at time cannot be known from the output of the downstream O 2 sensor 15 at time.

【0026】しかし、時刻から′に至る触媒コンバ
ータ下流側での空燃比変化(すなわち下流側O2 センサ
15の出力VO2の変化)は、時刻から時間dだけ遡っ
た時刻から時刻までの期間(〜の期間)におけ
る上流側空燃比A/Fの変化に対応しているのであるか
ら、〜の期間の上流側空燃比A/Fの変化履歴を知
れば′における触媒コンバータ下流の空燃比を推定す
ることが可能である。
However, the change in the air-fuel ratio on the downstream side of the catalytic converter (that is, the change in the output V O2 of the downstream side O 2 sensor 15) from the time to ′ is the period from the time to the time d traced back from the time by the time d. Since it corresponds to the change in the upstream side air-fuel ratio A / F during the period (-), the history of change in the upstream side air-fuel ratio A / F during the period (-) is used to estimate the air-fuel ratio downstream of the catalytic converter in ′. It is possible to

【0027】本実施例では、図3に示すように下流側O
2 センサ15の出力の一次遅れ系に近似した応答特性を
考慮して、上流側空燃比(上流側A/Fセンサ13の出
力信号)の、時間dだけ過去の時点から現在にいたるま
での期間の変動履歴と、現在の下流側O2 センサ15出
力値とを用いて現在から時間dだけ経過した時点の下流
側O2 センサ15出力値を以下の方法で推測する。
In this embodiment, as shown in FIG.
2 In consideration of the response characteristics approximate to the first-order lag system of the output of the sensor 15, the period from the time d of the upstream side air-fuel ratio (output signal of the upstream side A / F sensor 13) to the present time and variation history, guess downstream O 2 sensor 15 output value at the time that has elapsed since the current by time d in the following manner by using the current downstream O 2 sensor 15 output value.

【0028】まず、下流側O2 センサ15の出力を遅れ
時間dを有する一次遅れ系で近似して、時刻Kにおける
下流側O2 センサ出力VO2(K) と、直前の時刻(K−
1)における下流側O2 センサ出力VO2(K-1) 及び、時
刻(K−d)における上流側A/Fセンサ13の出力V
A/F(K-d)との関係を以下のモデル式で表す。 VO2(K) = α・VO2(K-1) + β・VA/F(K-d) ……(1) ここで、上記α、βは三元触媒の種類、下流側O2 セン
サの出力特性、サンプリング間隔(時刻K−1とKとの
時間間隔)等により決まる定数であり、実験により図3
の関係から予め算出しておく。(なお、α、βは定数と
せず下流側O2センサ15の出力に応じて変化するよう
に設定しても良い。)次いで、(1)式の関係を用い
て、以下の手順で、時刻Kにおける下流側O2センサ出
力VO2(K) から、時間d経過後の時刻(K+d)におけ
る下流側O2 センサ出力VO2(K+d) を推測する。
First, the output of the downstream O 2 sensor 15 is approximated by a first-order lag system having a delay time d, and the downstream O 2 sensor output V O2 (K) at time K and the immediately preceding time (K-
Downstream O 2 sensor output V O2 (K-1) in 1) and upstream A / F sensor 13 output V at time (Kd)
The relationship with A / F (Kd) is expressed by the following model formula. V O2 (K) = α · V O2 (K-1) + β · V A / F (Kd) (1) where α and β are three-way catalyst type and downstream O 2 sensor It is a constant determined by the output characteristics, sampling interval (time interval between time K-1 and K), etc.
It is calculated in advance from the relationship. (Note that α and β may not be constants and may be set so as to change according to the output of the downstream O 2 sensor 15.) Next, using the relationship of the equation (1), the time is calculated by the following procedure. from the downstream O 2 sensor output V O2 (K) in K, guess downstream O 2 sensor output V O2 (K + d) in the time after the time d has elapsed (K + d).

【0029】 《VO2(K+1) 》=α・VO2(K) +β・VA/F(K-d+1) …(21) 《VO2(K+2) 》=α・《VO2(K+1) 》+β・VA/F(K-d+2) …(22) 《VO2(K+3) 》=α・《VO2(K+2) 》+β・VA/F(K-d+3) …(23) ………………………………………………………… ………………………………………………………… 《VO2(K+d) 》=α・《VO2(K+d-1) 》+β・VA/F(K) …(2d)<< V O2 (K + 1) >> = α * VO2 (K) + β * VA / F (K-d + 1) (21) << VO2 (K + 2) >> = α * V O2 (K + 1) >> + β ・ V A / F (K-d + 2) … (22) 《V O2 (K + 3) 》 = α ・ 《V O2 (K + 2) 》 + β ・ V A / F (K-d + 3) … (23) ………………………………………………………………………………………………………… ………………… 《V O2 (K + d) 》 = α ・ 《V O2 (K + d-1) 》 + β ・ V A / F (K) … (2d)

【0030】ここで《VO2(i) 》(すなわち、《V
O2(K+1) 》、《VO2(K+2) 》、……、《VO2(K+d) 》)
は、それぞれ(1)式の関係を用いて求めた各時刻にお
ける下流側O2 センサ出力の推定値を表す。またV
A/F(i)(すなわちVA/F(K-d+1)、VA/F(K-d+2)、……、
A/F(K))は、上流側A/Fセンサ出力の実測値であ
る。
Here, << V O2 (i) >> (that is, << V
O2 (K + 1) >>, << VO2 (K + 2) >>, ..., << VO2 (K + d) >>)
Represents the estimated value of the downstream O 2 sensor output at each time, which is obtained by using the relationship of the equation (1). Also V
A / F (i) (that is, V A / F (K-d + 1) , V A / F (K-d + 2) , ...,
V A / F (K) ) is the actual measured value of the upstream A / F sensor output.

【0031】このようにして、過去の所定期間dの上流
側A/Fセンサ13の出力変化の履歴(実測値)と現在
の下流側O2 センサ15の出力(実測値)から時間d経
過後の下流側O2 センサ出力を高精度に推定することが
可能になる。次に、上記により求めた推定値《V
O2(K+d) 》に基づいた上流側A/Fセンサ13の出力の
補正について説明する。後述のように、本実施例では機
関燃焼空燃比は上流側A/Fセンサ13の出力に基づい
て理論空燃比にフィードバック制御される。このため、
上流側A/Fセンサ13の劣化による出力特性の変化
や、排気ガスの混合の不均一などにより上流側A/Fセ
ンサ13の出力が正確に排気空燃比を反映しなくなった
ような場合には空燃比制御が理論空燃比から外れ、運転
性が悪化したり三元触媒の排気浄化作用が維持できなく
なることになる。
In this way, after a lapse of time d from the history (measured value) of the output change of the upstream A / F sensor 13 in the past predetermined period d and the current output (measured value) of the downstream O 2 sensor 15. It becomes possible to highly accurately estimate the output of the downstream O 2 sensor. Next, the estimated value << V obtained above
The correction of the output of the upstream A / F sensor 13 based on O2 (K + d) >> will be described. As will be described later, in this embodiment, the engine combustion air-fuel ratio is feedback-controlled to the stoichiometric air-fuel ratio based on the output of the upstream side A / F sensor 13. For this reason,
When the output of the upstream A / F sensor 13 does not accurately reflect the exhaust air-fuel ratio due to a change in output characteristics due to deterioration of the upstream A / F sensor 13 or non-uniform mixing of exhaust gas The air-fuel ratio control deviates from the stoichiometric air-fuel ratio, which deteriorates drivability and makes it impossible to maintain the exhaust gas purification action of the three-way catalyst.

【0032】本実施例では、上記推定値《VO2(K+d)
と下流側O2 センサ15の理論空燃比相当出力VO2S と
の差、すなわちO2 ストレージ作用がなかったと仮定し
た場合に、現在の上流側排気が触媒コンバータを通過し
た時の触媒コンバータ下流側での排気空燃比の理論空燃
比からの偏差に基づいて、現在の上流側A/Fセンサ1
3出力VA/F(K)の補正を行う。 すなわち、触媒コンバ
ータ下流側での排気空燃比と理論空燃比との上記偏差が
ゼロになる方向に空燃比制御が行われるように上流側A
/Fセンサ13の出力を補正する。これにより、上流側
A/Fセンサ13の出力特性が変化したような場合で
も、上流側A/Fセンサの出力は直ちに補正され、機関
燃焼空燃比は常に理論空燃比に保たれることになる。
In this embodiment, the estimated value << V O2 (K + d) >>
And the theoretical air-fuel ratio equivalent output V O2 S of the downstream side O 2 sensor 15, that is, assuming that there is no O 2 storage action, the downstream side of the catalytic converter when the current upstream side exhaust gas passes through the catalytic converter. Based on the deviation of the exhaust air-fuel ratio from the stoichiometric air-fuel ratio at the current upstream side A / F sensor 1
3 Output V A / F (K) is corrected. That is, the upstream side A is controlled so that the air-fuel ratio control is performed in the direction in which the deviation between the exhaust air-fuel ratio and the stoichiometric air-fuel ratio on the downstream side of the catalytic converter becomes zero.
The output of the / F sensor 13 is corrected. As a result, even if the output characteristic of the upstream A / F sensor 13 changes, the output of the upstream A / F sensor is immediately corrected and the engine combustion air-fuel ratio is always kept at the theoretical air-fuel ratio. .

【0033】本実施例では、以下に示す補正値ΔV
A/F(K)を算出し、上流側A/Fセンサ13の現在出力V
A/F(K)に補正値ΔVA/F(K)を加算することにより上流側
A/Fセンサ13の出力補正を行う。
In this embodiment, the following correction value ΔV
A / F (K) is calculated and the current output V of the upstream A / F sensor 13
Performing output correction of the upstream A / F sensor 13 by adding the correction value [Delta] V A / F (K) to the A / F (K).

【0034】 ΔVA/F(K)= G1 ・Δ《VO2(K+d) 》 +G2 ・( i=0ΣK ΔVO2(i) i=K+1ΣK+d Δ《VO2(i) 》) +G3 ・(Δ《VO2(K+d) 》−Δ《VO2(K+d-1) 》)……(3) 及び、 *VA/F(K)=VA/F(K)+ΔVA/F(K) ……(4) ここで、*VA/F(K)は時刻Kにおける補正後の上流側A
/Fセンサ出力を、Δ《VO2(i) 》(i=K+1、K+
2、K+3、……、K+d)は、推定値《V O2(i) 》と
下流側O2 センサの理論空燃比相当出力電圧VO2S との
偏差を表す。すなわち、Δ《VO2(i) 》=
(《VO2(i) 》−VO2S )である。
ΔVA / F (K)= G1・ Δ << VO2 (K + d)>> + G2・ (i = 0ΣKΔVO2 (i)+i = K + 1ΣK + dΔ << VO2 (i)>>) + G3・ (Δ << VO2 (K + d)>>-Δ << VO2 (K + d-1)>>) …… (3) and * VA / F (K)= VA / F (K)+ ΔVA / F (K) (4) where * VA / F (K)Is the upstream side A after correction at time K
/ F sensor output, Δ << VO2 (i)>> (i = K + 1, K +
2, K + 3, ..., K + d) is an estimated value << V O2 (i)"When
Downstream O2Output voltage V equivalent to theoretical air-fuel ratio of sensorO2With S
Represents the deviation. That is, Δ << VO2 (i)>>
(<< VO2 (i)>>-VO2S).

【0035】また、 i=0ΣK ΔVO2(i) は、下流側O2
センサ出力の実測値VO2とVO2S との偏差ΔVO2の、時
刻ゼロ(機関始動時)から現在時刻Kまでの総和(積分
値)、 i=K+1ΣK+d Δ《VO2(i) 》は同様に、推定値
《VO2》の偏差Δ《VO2》についての時刻K+1からK
+dまでの総和(積分値)を表す。また、(Δ《V
O2(K+d) 》−Δ《VO2(K+d-1) 》)は時刻K+dにおけ
る上記偏差(推定値)の変化率を表す。すなわち、上記
により補正量ΔVA/F(K)は、下流側O2 センサ出力と理
論空燃比相当値との偏差に基づくPID(比例、積分、
微分)処理により決定される。ここで、G1 、G2 、G
3 はフィードバックのゲイン定数であり、実験等により
決定される。
Further, i = 0 Σ K ΔV O2 (i) is the downstream O 2
The sensor output measured value V O2 and V O2 S and deviation [Delta] V O2 of the sum from time zero (the time of engine startup) to the current time K (integral value), i = K + 1 Σ K + d Δ "V O2 (i) "likewise estimate" K from time K + 1 for V O2 "" deviation Δ of "V O2
It represents the total sum (integral value) up to + d. Also, (Δ << V
O2 (K + d) >>-[Delta] < VO2 (K + d-1) >>) represents the rate of change of the deviation (estimated value) at time K + d. That is, according to the above, the correction amount ΔV A / F (K) is determined by the PID (proportional, integral, PID) based on the deviation between the downstream O 2 sensor output and the stoichiometric air-fuel ratio equivalent value.
Differentiation) processing. Where G 1 , G 2 , G
3 is a feedback gain constant, which is determined by experiments and the like.

【0036】図4は制御回路10により実行される下流
側O2 センサ出力15の推定値の算出と、それに基づく
上流側A/Fセンサ13の出力の補正のルーチンを示す
フローチャートである。本ルーチンはクランク軸の一定
回転角毎に(例えば180度回転毎に)実行される。図
4においてルーチンがスタートすると、ステップ401
では上流側A/Fセンサ13と下流側O2 センサ15と
からそれぞれ出力VA/F 、VO2がA/D変換されて読み
込まれる。次いでステップ403では上記出力VA/F
O2を用いてVA/F 、VO2の現在値VA/F(K)、VO2(K)
が更新される。
FIG. 4 is a flow chart showing a routine executed by the control circuit 10 for calculating an estimated value of the downstream O 2 sensor output 15 and correcting the output of the upstream A / F sensor 13 based on the estimated value. This routine is executed every constant rotation angle of the crankshaft (for example, every 180 ° rotation). When the routine starts in FIG. 4, step 401
Then, the outputs V A / F and V O2 are respectively A / D converted and read from the upstream A / F sensor 13 and the downstream O 2 sensor 15. Next, at step 403, the output V A / F ,
With V O2 V A / F, the current value of V O2 V A / F (K ), V O2 (K)
Will be updated.

【0037】次いでステップ405では、上記の現在値
A/F(K)、VO2(K) を用いて、前述の式(21)〜(2
d)から推定値《VO2(K+1) 》〜《VO2(K+d) 》が演算
され、ステップ407では実測値VO2(K) と推定値《V
O2(K+1) 》〜《VO2(K+d) 》の理論空燃比相当出力VO2
S との偏差、それぞれΔVO2(K) 、Δ《VO2(K+1) 》〜
Δ《VO2(K+d) 》が演算される。
Next, at step 405, using the above current values V A / F (K) and V O2 (K) , the above equations (21) to (2 ) are used.
The estimated values << VO2 (K + 1) >> to << VO2 (K + d) >> are calculated from d) , and in step 407 the measured value VO2 (K) and the estimated value << VO2 (K)
O2 (K + 1) >> to << VO2 (K + d) >> theoretical air-fuel ratio equivalent output VO2
Deviation from S, ΔV O2 (K) , Δ << V O2 (K + 1) >>
Δ << VO2 (K + d) >> is calculated.

【0038】また、ステップ409ではVO2の実測値に
基づく偏差ΔVO2の時刻ゼロ(機関始動時)から現在時
刻Kまでの総和(積分値)、 i=0ΣK ΔVO2(i) が演算
されて、変数SUMとしてRAMに記憶され、ステップ
410ではVO2の推定値に基づく時刻K+1から時刻K
+dまでの偏差Δ《VO2(K+1) 》〜Δ《VO2(K+d) 》の
総和(積分値)、 i=K+1ΣK+d Δ《VO2(i) 》が演算さ
れ、変数《SUM》としてRAMに記憶される。
Further, the sum of the time zero deviation [Delta] V O2 based on the measured values of step 409 in V O2 (when starting the engine) to the current time K (integral value), i = 0 Σ K ΔV O2 (i) is operational Stored in the RAM as a variable SUM, and in step 410, time K + 1 to time K based on the estimated value of V O2.
+ Deviation Δ "V O2 (K + 1 )" to d ~Deruta sum of "V O2 (K + d) " ( integral value), i = K + 1 Σ K + d Δ "V O2 (i)" is It is calculated and stored in the RAM as a variable << SUM >>.

【0039】次いで、ステップ411では前述の(3)
式から補正量ΔVA/F(K)が計算され、ステップ413で
は前述の(4)式から補正後の上流側A/Fセンサ出
力、*VA/F(K)が算出される。さらに、ステップ415
では、次回のルーチン実行に備えてVA/F(K-d+1)からV
A/F(K-1)の値が更新され、その後ルーチンを終了する。
なお、本ルーチンでは、dは遅れ時間に相当するルーチ
ン実行回数であり、例えばd=2〜4程度とされる。す
なわち、本ルーチンではクランク軸の1〜2回転後の下
流側O2 センサ15の出力を常に予測して上流側A/F
センサ13の出力補正を行っている。
Then, in step 411, the above (3)
The correction amount ΔV A / F (K) is calculated from the equation, and in step 413, the corrected upstream A / F sensor output, * V A / F (K) is calculated from the above equation (4). Further, step 415
Then, from V A / F (K-d + 1) to V in preparation for the next routine execution
The value of A / F (K-1) is updated, and then the routine ends.
In this routine, d is the number of times the routine is executed corresponding to the delay time, and is set to, for example, d = 2 to 4. That is, in this routine, the output of the downstream O 2 sensor 15 after one or two rotations of the crankshaft is always predicted to predict the upstream A / F.
The output of the sensor 13 is corrected.

【0040】次に、上記により補正された上流側A/F
センサ13の出力*VA/F に基づく空燃比制御について
説明する。上流側A/Fセンサの出力信号に基づく空燃
比制御の方法には種々のものがあるが、ここでは三元触
媒のO2 ストレージ作用を最大限に活用するために、三
元触媒に吸着(貯蔵)された酸素量を所定量に維持する
ことを考慮しながら機関燃焼空燃比を理論空燃比に高精
度に短時間で収束させることが可能な、現代制御に基づ
く空燃比制御法に例をとって説明する。なお、本願出願
人は特願平5−68391号において既にこの空燃比制
御方法を提案している。
Next, the upstream A / F corrected as described above
The air-fuel ratio control based on the output * V A / F of the sensor 13 will be described. There are various methods of controlling the air-fuel ratio based on the output signal of the upstream side A / F sensor, but here, in order to make the most of the O 2 storage action of the three-way catalyst, adsorption ( An example of an air-fuel ratio control method based on modern control that allows the engine combustion air-fuel ratio to converge to the stoichiometric air-fuel ratio with high accuracy and in a short time while keeping the stored amount of oxygen at a predetermined amount. I will explain. The applicant of the present application has already proposed this air-fuel ratio control method in Japanese Patent Application No. 5-68391.

【0041】この空燃比制御方法では、エアフローメー
タ3の出力とエンジン回転数とからエンジン1回転当た
りに気筒内に吸入される空気量(気筒内空気量)mc
を、また、補正後の上流側A/Fセンサ13の出力*V
A/F から燃焼空燃比αを求め、これらから実際に気筒内
に供給された燃料量fcを、fc=mc/αとして算出
する。また、同様に理論空燃比αrを用いて燃焼空燃比
を理論空燃比にするために必要とされる目標燃料量fc
rをfcr=mc/αrとして算出し、これらの差fc
−fcr及び、その時間積分値x1を同時にゼロとする
ように燃料噴射量fiが決定される。
In this air-fuel ratio control method, the amount of air taken into the cylinder per engine revolution (the amount of air in the cylinder) mc is determined from the output of the air flow meter 3 and the engine speed.
And the corrected output * V of the upstream A / F sensor 13
The combustion air-fuel ratio α is obtained from the A / F, and the fuel amount fc actually supplied into the cylinder is calculated from these as fc = mc / α. Similarly, the target fuel amount fc required to make the combustion air-fuel ratio the stoichiometric air-fuel ratio by using the theoretical air-fuel ratio αr.
r is calculated as fcr = mc / αr, and the difference fc between them is calculated.
The fuel injection amount fi is determined so that −fcr and the time integrated value x1 thereof become zero at the same time.

【0042】また、燃料噴射弁7から噴射された燃料の
一部が吸気ポート壁面に付着するため、必ずしも燃料噴
射弁7からの噴射量と気筒内に供給される燃料量とは必
ずしも一致しないが、上記燃料噴射量fiの決定に際し
てはこの燃料付着が考慮される。上記のように目標値f
crからの実際の燃料供給量の偏差と、その時間積分値
とを同時にゼロにするように燃料噴射量fiを制御する
ことにより、三元触媒には常に所定の酸素量を貯蔵され
るとともに、空燃比制御の応答性を高めることができ
る。
Further, since a part of the fuel injected from the fuel injection valve 7 adheres to the wall surface of the intake port, the injection amount from the fuel injection valve 7 and the fuel amount supplied to the cylinder do not necessarily match. The fuel adhesion is taken into consideration when determining the fuel injection amount fi. As described above, the target value f
By controlling the fuel injection amount fi so that the deviation of the actual fuel supply amount from cr and the time integrated value thereof become zero at the same time, the three-way catalyst always stores a predetermined oxygen amount, and The responsiveness of air-fuel ratio control can be improved.

【0043】図5に上記の空燃比制御方法による燃料噴
射量(時間)fiの演算のフローチャートを示す。本ル
ーチンは、制御回路10により一定クランク回転角毎
(例えば360度回転毎)に実行される。図5において
ルーチンがスターとすると、ステップ501では、図4
のルーチンにより補正された上流側A/Fセンサ13の
出力*VA/F を用いて、図7の出力特性から空燃比αが
算出される。次いでステップ502、503では上記に
より求めた空燃比αとエアフローメータ3の出力とエン
ジン回転数とから求めたエンジン1回転当たりの吸入空
気量mc、及び理論空燃比αr(定数)とから、実際に
気筒内に供給された燃料量fcと、目標燃料量fcrと
が算出される。また、ステップ504では上記fcとf
crとの偏差δfcが、δfc=fc−fcrとして算
出される。
FIG. 5 shows a flow chart for calculating the fuel injection amount (time) fi by the above air-fuel ratio control method. This routine is executed by the control circuit 10 at every constant crank rotation angle (for example, every 360 ° rotation). If the routine is star in FIG. 5, in step 501, as shown in FIG.
The air-fuel ratio α is calculated from the output characteristic of FIG. 7 by using the output * V A / F of the upstream side A / F sensor 13 corrected by the routine of FIG. Next, at steps 502 and 503, from the air-fuel ratio α obtained above, the intake air amount mc per engine revolution obtained from the output of the air flow meter 3 and the engine speed, and the theoretical air-fuel ratio αr (constant), The fuel amount fc supplied to the cylinder and the target fuel amount fcr are calculated. In step 504, the above fc and f
The deviation δfc from cr is calculated as δfc = fc−fcr.

【0044】ステップ505では、燃料噴射量fiのノ
ミナル値fimが、 fim(k) ={fcr(k) −(1−P)fwm(k) }/
(1−R) として計算される。本実施例では、燃料噴射量fi、噴
射された燃料のうち吸気ポート壁面等に付着する燃料量
fw、気筒内に供給される燃料量fcは、それぞれノミ
ナル値fim、fwm、fcmと偏差δfi、δfw、
δfcとの和として以下のように表している。
In step 505, the nominal value fim of the fuel injection amount fi is fim (k) = {fcr (k) -(1-P) fwm (k) } /
Calculated as (1-R). In the present embodiment, the fuel injection amount fi, the fuel amount fw adhering to the wall surface of the intake port of the injected fuel, and the fuel amount fc supplied to the cylinders are the nominal values fim, fwm, fcm and the deviation δfi, respectively. δfw,
It is expressed as the sum of δfc as follows.

【0045】fi=fim+δfi fw=fwm+δfw fc=fcm+δfc また、これらの間には以下のモデル式が成立していると
仮定する。 fw(k+1) =Pfw(k) +Rfi(k) fc(k) =(1−P)fw(k) +(1−R)fi(k) fwm(k+1) =Pfwm(k) +Rfim(k) fcm(k) =(1−P)fwm(k) +(1−R)fim
(k) fcm(k) =fcr(k) ここで、添字kは今回ルーチン実行時の値を、(k−
1)は前回ルーチン実行時の値を示す。また、本実施例
ではP、Rは定数である。上記モデル式を変形してステ
ップ505ではノミナル値fimが上記の形として求め
られる。
Fi = fim + δfi fw = fwm + δfw fc = fcm + δfc It is also assumed that the following model formula is established between them. fw (k + 1) = Pfw (k) + Rfi (k) fc (k) = (1-P) fw (k) + (1-R) fi (k) fwm (k + 1) = Pfwm (k) + Rfim (k) fcm (k) = (1-P) fwm (k) + (1-R) fim
(k) fcm (k) = fcr (k) where the subscript k is the value at the time of execution of this routine, (k-
1) indicates the value at the time of executing the previous routine. Further, in this embodiment, P and R are constants. By modifying the above model equation, in step 505 the nominal value fim is obtained in the above form.

【0046】次いでステップ506では、δfcの時間
積分値x1が、x1(k) =x1(k-1) +δfc(k)
して、また、ステップ507では更にx1の時間積分値
x2が、x2(k) =x2(k-1) +x1(k) として求
められる。更に、ステップ508では、前回までに求め
たfi、δfc、x1、x2等の値を用いて偏差δfi
が、 δfi(k) =f1・δfi(k-1) +f2・δfc(k-1) +f3・x1(k) +f4・x1(k-1) +f5・x1(k-2) +f6・x2(k-1) +f7・x2(k-2) として計算される。ここで、f1からf7は定数であ
る。
Next, at step 506, the time integral value x1 of δfc is set to x1 (k) = x1 (k-1) + δfc (k) , and at step 507, the time integral value x2 of x1 is further changed to x2 (k ) = X2 (k-1) + x1 (k) . Further, in step 508, the deviation δfi is calculated using the values of fi, δfc, x1, x2, etc. obtained up to the previous time.
, Δfi (k) = f1 · δfi (k-1) + f2 · δfc (k-1) + f3 · x1 (k) + f4 · x1 (k-1) + f5 · x1 (k-2) + f6 · x2 (k -1) Calculated as + f7 · x2 (k-2) . Here, f1 to f7 are constants.

【0047】ステップ509では、上記によりもとめた
燃料噴射量のノミナル値fimと偏差δfiとを用いて
燃料噴射量fiが、fi(k) =fim(k) +δfi(k)
として求められる。また、ステップ510では、次回の
ルーチン実行に備えて、壁面付着燃料量のノミナル値が
今回ルーチン実行時のfwmとRfimとの値を用い
て、fwm=Pfwm(k) +Rfim(k) として計算さ
れ、ステップ511から516では、次回のルーチン実
行に備えて、δfi(k-1) 、δfc(k-1) 、x
(k-1) 、x1(k-2) 、x2(k-1) 、x2(k-2) の値が
それぞれ今回ルーチン実行時の値を用いて更新される。
In step 509, the fuel injection amount fi is determined as fi (k) = fim (k) + δfi (k) using the nominal value fim of the fuel injection amount and the deviation δfi obtained as described above.
Is required as. Further, in step 510, in preparation for the next routine execution, the nominal value of the amount of fuel adhering to the wall surface is calculated as fwm = Pfwm (k) + Rfim (k) using the values of fwm and Rfim at the time of execution of this routine. In steps 511 to 516, δfi (k-1) , δfc (k-1) , x are prepared for the next routine execution.
The values of 1 (k-1) , x1 (k-2) , x2 (k-1) , and x2 (k-2) are updated using the values at the time of execution of this routine.

【0048】上記により、燃料噴射量(噴射時間)fi
が決定されると、別途実行される燃料噴射ルーチン(図
示せず)により、制御回路10のダウンカウンタ108
に時間fiがセットされ、駆動回路110により燃料噴
射弁7からfiに相当する量の燃料が噴射される。上述
のルーチンによれば、下流側O2 センサ15の出力の将
来の予測値を用いて補正した上流側A/Fセンサ13の
出力に基づいて燃料噴射量の制御がおこなわれるため、
空燃比の理論空燃比からのずれは極めて早く補正され、
常に高精度の制御が行われる。
From the above, the fuel injection amount (injection time) fi
Is determined, a down-counter 108 of the control circuit 10 is executed by a fuel injection routine (not shown) executed separately.
Is set to the time fi, and the drive circuit 110 injects fuel from the fuel injection valve 7 in an amount corresponding to fi. According to the above-described routine, the fuel injection amount is controlled based on the output of the upstream A / F sensor 13 corrected using the future predicted value of the output of the downstream O 2 sensor 15.
The deviation of the air-fuel ratio from the theoretical air-fuel ratio is corrected very quickly,
High precision control is always performed.

【0049】[0049]

【発明の効果】本発明によれば、上流側空燃比センサの
出力信号の過去所定期間の変化履歴と、下流側空燃比セ
ンサの現在の出力信号とを用いて、現在から所定時間が
経過した時点の下流側空燃比センサの出力信号を推定
し、この推定値に基づいて上流側空燃比センサ出力を補
正するようにしたことにより、下流側空燃比センサ出力
の時間遅れによる空燃比制御の応答性悪化を防止し、高
精度で応答性の良好な空燃比制御を行うことが可能とな
る効果を奏する。
According to the present invention, a predetermined time has elapsed from the present using the change history of the output signal of the upstream side air-fuel ratio sensor in the past predetermined period and the present output signal of the downstream side air-fuel ratio sensor. The output signal of the downstream side air-fuel ratio sensor is estimated at this time, and the upstream side air-fuel ratio sensor output is corrected based on this estimated value, so that the response of the air-fuel ratio control due to the time delay of the downstream side air-fuel ratio sensor output As a result, it is possible to prevent deterioration of performance and perform air-fuel ratio control with high accuracy and good responsiveness.

【図面の簡単な説明】[Brief description of drawings]

【図1】本発明の構成を示すブロック図である。FIG. 1 is a block diagram showing a configuration of the present invention.

【図2】本発明の一実施例を適用した内燃機関の全体図
である。
FIG. 2 is an overall view of an internal combustion engine to which an embodiment of the present invention is applied.

【図3】下流側O2 センサの出力の将来値の推定方法を
説明するための図である。
FIG. 3 is a diagram for explaining a method of estimating a future value of an output of a downstream O 2 sensor.

【図4】下流側O2 センサの出力推定と上流側A/Fセ
ンサの出力補正を行うためのルーチンのフローチャート
である。
FIG. 4 is a flowchart of a routine for estimating output of a downstream O 2 sensor and correcting output of an upstream A / F sensor.

【図5】上流側A/Fセンサの出力に基づく空燃比フィ
ードバック制御ルーチンのフローチャートである。
FIG. 5 is a flowchart of an air-fuel ratio feedback control routine based on the output of the upstream A / F sensor.

【図6】A/Fセンサの一般的構造を説明するための図
である。
FIG. 6 is a diagram for explaining a general structure of an A / F sensor.

【図7】上流側A/Fセンサの出力特性の一例を示す図
である。
FIG. 7 is a diagram showing an example of output characteristics of an upstream A / F sensor.

【図8】下流側O2 センサの出力特性の一例を示す図で
ある。
FIG. 8 is a diagram showing an example of output characteristics of a downstream O 2 sensor.

【符号の説明】[Explanation of symbols]

1…機関本体 2…吸気通路 3…エアフローメータ 7…燃料噴射弁 10…制御回路、 12…触媒コンバータ 13…上流側空燃比センサ 15…下流側空燃比センサ DESCRIPTION OF SYMBOLS 1 ... Engine main body 2 ... Intake passage 3 ... Air flow meter 7 ... Fuel injection valve 10 ... Control circuit 12 ... Catalytic converter 13 ... Upstream air-fuel ratio sensor 15 ... Downstream air-fuel ratio sensor

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 内燃機関の排気通路に配置された三元触
媒と、該三元触媒の上流側排気通路に配置され排気空燃
比に応じた出力信号を発生する上流側空燃比センサと、
前記三元触媒の下流側排気通路に配置され排気空燃比に
応じた出力信号を発生する下流側空燃比センサと、 前記上流側空燃比センサの出力信号の過去所定期間の変
化履歴と、前記下流側空燃比センサの現在の出力信号と
に基づいて、現在から所定時間経過後の前記下流側空燃
比センサの出力信号の将来値を推定する推定手段と、 前記推定された下流側空燃比センサの出力信号に基づい
て前記上流側空燃比センサの現在の出力を補正する補正
手段と、 前記補正された上流側空燃比センサの出力に基づいて前
記内燃機関の燃焼空燃比を制御する制御手段とを備えた
内燃機関の空燃比制御装置。
1. A three-way catalyst arranged in an exhaust passage of an internal combustion engine, and an upstream air-fuel ratio sensor arranged in an upstream exhaust passage of the three-way catalyst for generating an output signal according to an exhaust air-fuel ratio,
A downstream side air-fuel ratio sensor which is arranged in a downstream side exhaust passage of the three-way catalyst and generates an output signal according to an exhaust air-fuel ratio, a change history of a past predetermined period of an output signal of the upstream side air-fuel ratio sensor, and the downstream side Based on the current output signal of the side air-fuel ratio sensor, an estimating means for estimating a future value of the output signal of the downstream side air-fuel ratio sensor after a predetermined time has elapsed from the present, and the estimated downstream side air-fuel ratio sensor Correcting means for correcting the current output of the upstream side air-fuel ratio sensor based on the output signal, and control means for controlling the combustion air-fuel ratio of the internal combustion engine based on the corrected output of the upstream side air-fuel ratio sensor. An internal-combustion engine air-fuel ratio control device equipped with.
JP05234950A 1993-09-21 1993-09-21 Air-fuel ratio control device for internal combustion engine Expired - Fee Related JP3134624B2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP05234950A JP3134624B2 (en) 1993-09-21 1993-09-21 Air-fuel ratio control device for internal combustion engine
US08/305,641 US5475975A (en) 1993-09-21 1994-09-14 Air-fuel ratio control device for an engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP05234950A JP3134624B2 (en) 1993-09-21 1993-09-21 Air-fuel ratio control device for internal combustion engine

Publications (2)

Publication Number Publication Date
JPH0791297A true JPH0791297A (en) 1995-04-04
JP3134624B2 JP3134624B2 (en) 2001-02-13

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ID=16978804

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Status (2)

Country Link
US (1) US5475975A (en)
JP (1) JP3134624B2 (en)

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US5475975A (en) 1995-12-19

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